Skip to content
Home Library Satellite Directory N-1 DEB

N-1 DEB

NORAD 13510 Debris LEO 1982-087C
CONNECTING… LEO · NORAD 13510
NOW PASSING OVER
Calculating position…
Altitude (km)
Speed (km/s)
Latitude
Longitude
Real-time tracking powered by Orbital Radar
ORBITAL RADAR · LIVE GROUND TRACK
🌍 Track on 3D Globe
🛰️ Orbital Parameters
Perigee
917 km
Apogee
1159 km
Inclination
44.6°
Period
105.9 min
Mean Motion
13.59357564 rev/day
TLE Epoch
2026-06-07 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,038 km
Orbital Velocity26,405 km/h
Velocity7.33 km/s
Orbital Period106 minutes
Orbits / Day13.59
Eccentricity0.0163
Semi-Major Axis7,409 km
Est. Orbital Lifetime~500–1,000 years
🚀 Launch & Identity
Country / Operator
🇯🇵 Japan
Launch Date
1982-09-03
Launch Site
TNSTA
Int'l Designator
1982-087C
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
N-1 DEB is a tracked piece of space debris attributed to Japan, launched on 1982-09-03 from TNSTA. With over 44 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 917 km and 1,159 km with an inclination of 44.6°. It travels at approximately 26,405 km/h (7.33 km/s), completing one full orbit every 106 minutes — that’s roughly 13.59 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~500–1,000 years. As orbital debris, N-1 DEB poses a potential collision risk to operational satellites in nearby orbits and is continuously monitored by the U.S. Space Surveillance Network and other tracking systems.
🌍 Orbit Context
N-1 DEB orbits at an average altitude of 1,038 km in the upper LEO band, where atmospheric drag is negligible and objects can persist for centuries to millennia. This altitude is used by broadband constellations like OneWeb and by scientific missions requiring stable orbits far from the densest debris bands. Within ±50 km of N-1 DEB’s average altitude, there are currently 183 active payloads and 501 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0041. With an inclination of 44.6°, N-1 DEB passes over latitudes between 44.6°N and 44.6°S, covering the tropical and temperate zones where most of the world’s population resides. Low-to-mid inclination orbits are efficient to reach from equatorial and mid-latitude launch sites. Japan operates approximately 189 active satellites in total, of which 4 share a similar altitude band with N-1 DEB.
🔗 Tracked Space Debris

This is a tracked piece of orbital debris — a fragment from a collision, explosion, or separation event that no longer serves any useful purpose. Space surveillance networks catalogue objects larger than approximately 10 cm in LEO. Even small debris can be catastrophic at orbital velocities (7–8 km/s in LEO), carrying kinetic energy comparable to a hand grenade per centimetre-sized fragment. The growing debris population is one of the most pressing challenges for long-term space sustainability.

❓ Frequently Asked Questions
N-1 DEB orbits in Low Earth Orbit (LEO) at altitudes between 917 km (perigee) and 1,159 km (apogee), with an average altitude of approximately 1,038 km. It completes one orbit every 106 minutes, travelling at approximately 26,405 km/h (16,408 mph).
N-1 DEB (NORAD ID 13510) is a piece of tracked orbital debris attributed to Japan. It was likely created by a fragmentation event, collision, or mission-related separation. Even small debris objects at orbital velocities carry enormous kinetic energy, so they are tracked by the U.S. Space Surveillance Network to enable collision avoidance for operational satellites.
N-1 DEB was launched on 1982-09-03 from TNSTA. At its current altitude, the estimated remaining orbital lifetime is: ~500–1,000 years. View the full satellite launch log.
Yes — Orbital Radar tracks N-1 DEB (NORAD ID 13510) using the latest TLE (two-line element set) data from Space-Track and CelesTrak. Open the live tracker to see its current position, altitude, speed and orbital path updated in real time. You can also browse the satellite directory to find other tracked objects.
N-1 DEB travels at approximately 26,405 km/h (16,408 mph) — roughly 7.33 km/s. It completes 13.59 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 27 sunrises and sunsets every 24 hours.
All tracked debris poses a potential collision risk to operational satellites. At orbital velocities, even a small object carries enormous kinetic energy — a 1 cm fragment at 7.33 km/s has the energy equivalent of a hand grenade. Space agencies perform routine conjunction assessments and may manoeuvre operational satellites to avoid tracked objects like N-1 DEB. Read more about debris statistics and the Kessler syndrome.